What was found
DURING FLIGHT ILLUMINATION OF #2 ENGINE FUEL PRESSURE CAUTION LIGHT. NOTE: MULTIPLE ENGINE TORQUE SPLITS OCCURRED DURING CRUISE, AND LANDING. MANUAL CONTROL OF VARNAR REQUIRED TO MAINTAIN NORMAL AIRCRAFT LIMITS AND SAFE OPERATIONS. T/F EVAL: STEADY CRUISE FLIGHT AT 100 KIAS, 1500FT PA, #2 ENGINE HAD OSCILLATION FOLLOWED BY #2 FUEL PRESSURE LIGHT ILLUMINATED WITH #2 ENGINE DROPPING 30% TQ AND THEN RECOVERING WITH FUEL PRESSURE LIGHT GOING OFF. REPLACED FUEL CONTROL UNIT IAW SAFRAN HELICOPTERS ENGINE MAINT MANUAL 73-21-00-900-801-B01. MOC COMPLETED OK IAW AMM 05-60-00, 6-1.